Dual Radio Autopilot System for Lightweight, Swarming Micro/Miniature Aerial Vehicles
نویسندگان
چکیده
This paper presents the autonomous micro aerial vehicle pilot, a new autopilot platform weighing 6.25 g and measuring 11.3 cm2, specifically designed for use on micro/miniature aerial vehicle mobile sensing platforms. An overview of the hardware, firmware, ground station, and validation testing used to demonstrate this autopilot as a viable research instrument for atmospheric thermodynamic sensing on micro/miniature aerial vehicles is presented. The autonomous micro aerial vehicle pilot incorporates a 16 bit 140 MHz processor, global positioning system, dual radios, inertial measurement unit, pressure sensor, humidity sensor, and temperature sensor. Through these components, the autonomous micro aerial vehicle pilot is capable of full-state feedback, vehicle state estimation, localization, and wireless networking. Notable features of this autopilot are its dual-radio configuration, providing redundancy and adaptability in communication, and the detachable sensor breakout design that allows for increased flexibility in sensorplacement onavehicle. Full-state feedbackof the autopilot platformwasvalidated througha series of bench tests. This includes a unique technique for dynamic inertial measurement unit validation performed using the present group’s model positioning system as well as comparing estimated pressure values with known values at multiple heights and global positioning system values with a known path. Systemwide validation was performed through flight tests on a micro/miniature aerial vehicle airframe.
منابع مشابه
Autopilots for Small Unmanned Aerial Vehicles: A Survey
This paper presents a survey of the autopilot systems for small or micro unmanned aerial vehicles (UAVs). The objective is to provide a summary of the current commercial, open source and research autopilot systems for convenience of potential small UAV users. The UAV flight control basics are introduced first. The radio control system and autopilot control system are then explained from both th...
متن کاملAutonomous Navigation in a Warehouse with a Cognitive Micro Aerial Vehicle
Micro aerial vehicles (MAVs), such as multirotors, are envisioned for autonomous inventory-taking in large warehouses. Fully autonomous operation of MAVs in such complex 3D environments requires real-time state estimation, obstacle detection, mapping, and navigation planning. To this end, we employ a cognitive MAV equipped with multiple sensors including a dual 3D laser scanner, three stereo ca...
متن کاملA Small Semi-Autonomous Rotary-Wing Unmanned Air Vehicle (UAV)
Small radio controlled (R/C) rotary-wing UAVs have many potential military and civilian applications, but can be very difficult to fly. Small and lightweight sensors and computers can be used to implement a control system to make these vehicles easier to fly. To develop a control system for a small UAV, an 8-bit microcontroller has been interfaced with MEMS (Micro-Electro-Mechanical Systems) gy...
متن کاملVision-guided Control Algorithms for Micro Aerial Vehicles
This study presents an image analysis method used in the vision guided control system for Micro Air Vehicles (MAVs). The paper describes a hypothetical model of a MAV located in the GPS-denied unknown environment, somewhere indoors. The model keeps moving autonomously following ‘the track’ marked with corners and other feature points recorded with a monocular camera pointed at the far end of a ...
متن کاملOptic flow-based vision system for autonomous 3D localization and control of small aerial vehicles
The problem considered in this paper involves the design of a vision-based autopilot for small and micro Unmanned Aerial Vehicles (UAVs). The proposed autopilot is based on an optic flow-based vision system for autonomous localization and scene mapping, and a nonlinear control system for flight control and guidance. This paper focusses on the development of a real-time 3D vision algorithm for e...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید
ثبت ناماگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید
ورودعنوان ژورنال:
- J. Aerospace Inf. Sys.
دوره 14 شماره
صفحات -
تاریخ انتشار 2017